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    AIRCRAFT HOSE RETRIEVAL SYSTEM
    1.
    发明申请
    AIRCRAFT HOSE RETRIEVAL SYSTEM 失效
    飞机软管检索系统

    公开(公告)号：US20120042979A1

    公开(公告)日：2012-02-23

    申请号：US12860579

    申请日：2010-08-20

    申请人： Anatoly Gosis ,  Folkert Fred Koch ,  Frank Otte

    发明人： Anatoly Gosis ,  Folkert Fred Koch ,  Frank Otte

    IPC分类号： F16L3/00 ,  B65H75/34 ,  F16L11/00 ,  B66C1/42

    CPC分类号： B64F1/362 ,  Y10T137/6918 ,  Y10T137/6932

    摘要： The present embodiments are directed towards the transfer, retrieval and storage of flexible materials. In one embodiment, a system is provided that generally includes a hose retrieval system having a first hose gripper assembly. The first hose gripper assembly includes a pair of first grippers configured to move between a first open position and a first closed position in opposite crosswise directions relative to a longitudinal axis of a hose. Each first gripper includes a first L-shaped structure, and the first L-shaped structures are configured to overlap one another to define a first bending gap in the first closed position.

    摘要翻译： 本实施例涉及柔性材料的传送，检索和存储。 在一个实施例中，提供了一种系统，其通常包括具有第一软管夹持器组件的软管取回系统。 第一软管夹持器组件包括一对第一夹持器，其构造成相对于软管的纵向轴线在相反的横向方向上在第一打开位置和第一关闭位置之间移动。 每个第一夹持器包括第一L形结构，并且第一L形结构构造成彼此重叠以在第一关闭位置限定第一弯曲间隙。

    AIRCRAFT POWER CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES
    2.
    发明申请
    AIRCRAFT POWER CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES 有权
    具有差异接合和操作保持力的飞机电源连接器

    公开(公告)号：US20100029123A1

    公开(公告)日：2010-02-04

    申请号：US11681674

    申请日：2007-03-02

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Frank Otte ,  Dennis Bednarz

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Frank Otte ,  Dennis Bednarz

    IPC分类号： H01R13/62

    CPC分类号： H01R13/193 ,  H01R13/639

    摘要： A new and improved aircraft power connector, for electrical connection to an aircraft electrical connector, has incorporated thereon a dual-position mechanism which can effectively alter the engagement force level defined between the electrical connector contact pins of the aircraft power connector and the aircraft electrical connector. When the mechanism is disposed at a first position, the force level is relatively low so as to easily permit connection and disconnection, whereas when the mechanism is disposed at a second position, the force level is relatively high so as to ensure the connection of the aircraft power connector to the aircraft electrical connector and thereby prevent the inadvertent disconnection of the aircraft power connector from the aircraft electrical connector.

    摘要翻译： 用于电气连接到飞机电连接器的新的和改进的飞行器电源连接器已经结合有双位置机构，其可以有效地改变在飞行器电源连接器的电连接器接触销和飞行器电连接器之间限定的接合力水平 。 当机构设置在第一位置时，力水平相对较低，以便容易地允许连接和断开，而当机构设置在第二位置时，力水平相对较高，以确保连接 飞机电源连接器连接到飞机电连接器，从而防止飞机电源连接器与飞机电连接器的意外断开。

    Aircraft hose retrieval system
    3.
    发明授权
    Aircraft hose retrieval system 失效
    飞机软管检索系统

    公开(公告)号：US08459296B2

    公开(公告)日：2013-06-11

    申请号：US12860579

    申请日：2010-08-20

    申请人： Anatoly Gosis ,  Folkert Fred Koch ,  Frank Otte

    发明人： Anatoly Gosis ,  Folkert Fred Koch ,  Frank Otte

    IPC分类号： A62C35/00

    CPC分类号： B64F1/362 ,  Y10T137/6918 ,  Y10T137/6932

    摘要： The present embodiments are directed towards the transfer, retrieval and storage of flexible materials. In one embodiment, a system is provided that generally includes a hose retrieval system having a first hose gripper assembly. The first hose gripper assembly includes a pair of first grippers configured to move between a first open position and a first closed position in opposite crosswise directions relative to a longitudinal axis of a hose. Each first gripper includes a first L-shaped structure, and the first L-shaped structures are configured to overlap one another to define a first bending gap in the first closed position.

    摘要翻译： 本实施例涉及柔性材料的传送，检索和存储。 在一个实施例中，提供了一种系统，其通常包括具有第一软管夹持器组件的软管取回系统。 第一软管夹持器组件包括一对第一夹持器，其构造成相对于软管的纵向轴线在相反的横向方向上在第一打开位置和第一关闭位置之间移动。 每个第一夹持器包括第一L形结构，并且第一L形结构构造成彼此重叠以在第一关闭位置限定第一弯曲间隙。

    Aircraft power connector with differential engagement and operational retention forces
    4.
    发明授权
    Aircraft power connector with differential engagement and operational retention forces 有权
    具有差异接合和操作保持力的飞机电源连接器

    公开(公告)号：US07871282B2

    公开(公告)日：2011-01-18

    申请号：US11681674

    申请日：2007-03-02

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Frank Otte ,  Dennis Bednarz

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Frank Otte ,  Dennis Bednarz

    IPC分类号： H01R13/15

    CPC分类号： H01R13/193 ,  H01R13/639

    摘要： A new and improved aircraft power connector, for electrical connection to an aircraft electrical connector, has incorporated thereon a dual-position mechanism which can effectively alter the engagement force level defined between the electrical connector contact pins of the aircraft power connector and the aircraft electrical connector. When the mechanism is disposed at a first position, the force level is relatively low so as to easily permit connection and disconnection, whereas when the mechanism is disposed at a second position, the force level is relatively high so as to ensure the connection of the aircraft power connector to the aircraft electrical connector and thereby prevent the inadvertent disconnection of the aircraft power connector from the aircraft electrical connector.

    摘要翻译： 用于电气连接到飞机电连接器的新的和改进的飞行器电源连接器已经结合有双位置机构，其可以有效地改变在飞行器电源连接器的电连接器接触销和飞行器电连接器之间限定的接合力水平 。 当机构设置在第一位置时，力水平相对较低，以便容易地允许连接和断开，而当机构设置在第二位置时，力水平相对较高，以确保连接 飞机电源连接器连接到飞机电连接器，从而防止飞机电源连接器与飞机电连接器的意外断开。

    AIRBAG FASTENER ASSEMBLY
    5.
    发明申请
    AIRBAG FASTENER ASSEMBLY 有权
    安全气囊紧固件总成

    公开(公告)号：US20090285648A1

    公开(公告)日：2009-11-19

    申请号：US12409006

    申请日：2009-03-23

    申请人： Anatoly Gosis ,  Brock T. Cooley ,  James T. Kirchen ,  Frank Otte

    发明人： Anatoly Gosis ,  Brock T. Cooley ,  James T. Kirchen ,  Frank Otte

    IPC分类号： F16B13/04

    CPC分类号： B60R21/20 ,  B25B31/00 ,  B60R13/0206 ,  B60R21/213 ,  B60R21/232 ,  F16B19/1081 ,  Y10T24/309 ,  Y10T24/44026

    摘要： A fastener for securing an airbag assembly in a motor vehicle includes first and second body components held one against another with a fastening tab of an airbag there between. A flexible collet from the body of the fastener is secured in a hole of a supporting component in a vehicle roof, and a pin pushed into the collet secures the installation. Tools and fastener structures for verification testing are disclosed.

    摘要翻译： 用于将气囊组件固定在机动车辆中的紧固件包括彼此抵靠的第一和第二主体部件以及其间的气囊的紧固突出部。 来自紧固件主体的柔性夹头被固定在车顶中的支撑部件的孔中，并且被推入夹头的销固定安装。 公开了用于验证测试的工具和紧固件结构。

    System and Method For Controlling Temperature Indicators
    6.
    发明申请
    System and Method For Controlling Temperature Indicators 失效
    用于控制温度指示器的系统和方法

    公开(公告)号：US20080137713A1

    公开(公告)日：2008-06-12

    申请号：US12034956

    申请日：2008-02-21

    申请人： Anatoly Gosis ,  Shannon B. Reading ,  Joseph E. Fabin ,  Frank Otte

    发明人： Anatoly Gosis ,  Shannon B. Reading ,  Joseph E. Fabin ,  Frank Otte

    IPC分类号： G01K1/08

    CPC分类号： G01K11/06 ,  G01K1/146 ,  G01K11/12

    摘要： A system and method for controlling a temperature indicator stick includes a housing having an interior configured to receive the temperature indicator stick configured to indicate a predetermined temperature through a physical change or a chemical when exposed to the predetermined temperature. A roller drive is supported by the housing to engage the temperature indicator stick. Accordingly, rotation of the drive roller causes a retraction or advancement of the temperature indicator stick to and from the interior of the housing. Additionally, the housing and temperature indicator stick may include a key system to keep the temperature indicator stick in a substantially fixed rotational position with respect to the housing as the temperature indicator stick advanced from and retracted into the housing.

    摘要翻译： 用于控制温度指示器棒的系统和方法包括具有内部的壳体，所述内部构造成用于接收当暴露于预定温度时通过物理变化或化学物质指示预定温度的温度指示器棒。 辊子驱动器由壳体支撑以接合温度指示器棒。 因此，驱动辊的旋转导致温度指示器棒与壳体内部的退回或前进。 另外，壳体和温度指示器棒可以包括一个钥匙系统，当温度指示器杆从壳体前进并缩回到壳体中时，可将温度指示器保持在相对于壳体的基本上固定的旋转位置。

    Asymmetrical strap chute and release system
    7.
    发明授权
    Asymmetrical strap chute and release system 有权
    不对称带槽和释放系统

    公开(公告)号：US07237478B1

    公开(公告)日：2007-07-03

    申请号：US11461789

    申请日：2006-08-02

    申请人： Anatoly Gosis ,  Thomas A. Powers ,  Frank Otte ,  Yury Shkolnikov

    发明人： Anatoly Gosis ,  Thomas A. Powers ,  Frank Otte ,  Yury Shkolnikov

    IPC分类号： B65B13/04

    CPC分类号： B65B13/06

    摘要： An asymmetrical chute system is for use in a strapping machine of the type for feeding a strapping material around a load, positioning, tensioning and sealing the strapping material around the load. The strapping machine has a feed head, a strap chute defining a strap path through which the strapping material is passed and a sealing head. The chute system includes a base, a stationary guard having an inclined wall extending, at least in part, over the strap path and a movable guard. The movable guard is movable relative to the base and the stationary guard into and out of engagement with the stationary guard inclined wall to open and close the strap path. When the movable guard is open, the inclined wall extends over the strap path so as to form a blind portion intersecting a line normal to the strap path.

    摘要翻译： 不对称滑槽系统用于捆扎机的类型，用于将捆扎材料围绕负载进给，将捆扎材料定位，张紧和密封在负载周围。 捆扎机具有进料头，带状滑槽，其限定捆扎带通过的带通道和密封头。 滑槽系统包括底座，具有至少部分地在带路径上延伸的倾斜壁的固定护罩和可移动护罩。 可移动护罩可相对于基座和固定护罩移动，并与固定护罩倾斜壁接合，以打开和关闭吊带路径。 当可移动防护罩打开时，倾斜壁在带路径上延伸，以便形成与垂直于带路径的线相交的盲部。

    SYSTEM AND METHOD FOR MULTIPLE-TEMPERATURE INDICATOR STICK
    9.
    发明申请
    SYSTEM AND METHOD FOR MULTIPLE-TEMPERATURE INDICATOR STICK 失效
    多温度指示器系统和方法

    公开(公告)号：US20080107153A1

    公开(公告)日：2008-05-08

    申请号：US11556376

    申请日：2006-11-03

    申请人： Anatoly Gosis ,  Shannon B. Reading ,  Joseph E. Fabin ,  Frank Otte

    发明人： Anatoly Gosis ,  Shannon B. Reading ,  Joseph E. Fabin ,  Frank Otte

    IPC分类号： G01K11/12 ,  G01K1/00 ,  G01K11/00 ,  G01K11/06

    CPC分类号： G01K11/06 ,  G01K11/12

    摘要： A system and method for a multi-temperature indicator stick. The multi-temperature indicator stick includes an elongated stick configured to indicate two or more predetermined temperatures. The elongated stick includes a first temperature indication material configured to indicate a first predetermined temperature upon being subjected to the first predetermined temperature. The elongated stick also includes a second temperature indication material configured to indicate a second predetermined temperature upon being subjected to the second predetermined temperature. The first temperature indication material and the second temperature indication material share a common interface extending longitudinally along the elongated stick.

    摘要翻译： 一种多温度指示棒的系统和方法。 多温度指示棒包括被配置为指示两个或更多个预定温度的细长棒。 细长棒包括构造成在经受第一预定温度时指示第一预定温度的第一温度指示材料。 细长棒还包括构造成在经受第二预定温度时指示第二预定温度的第二温度指示材料。 第一温度指示材料和第二温度指示材料共享沿着细长棒纵向延伸的公共界面。